Experimental investigations of simulated meteoroid damage to various spacecraft structures Summary report
Optimum structural meteoroid protection requirements for Apollo and Mars mission spacecraft
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Optimum structural meteoroid protection requirements for Apollo and Mars mission spacecraft
Impact calibration tests in development of meteoroid penetration distributed transducer
Photographic observations of low density iron artificial meteoroid
Meteoroid impact damage to Apollo and Gemini ablative heat shields
Scaling laws for predicting penetration of semiinfinite targets by particles traveling at meteoroid velocities - simulation techniques for low velocity and hypervelocity impacts
Electron irradiation from 20 keV to 1 MeV used to study effects on polyethylene terephthalate capacitor-type meteoroid detector
Material and geometry aspects of meteoroid armor protection for space radiator tubes, discussing bumper-fin concept
Model of near-earth meteoroid environment from satellite observation data
Satellite instrumentation and data retrieval procedures for collecting meteoroid penetration data from Pegasus satellite
Data collection and analysis of meteoroid penetration recorded on Pegasus flights, and derived flux figures
Statistical analysis of Pegasus satellite measurements of meteoroid penetration
Meteoroid hazards to solid propellant rocket motors
Mathematical model for determining ballistic limit of double-walled meteoroid bumper systems
Impact effects applied to meteoroid hazard
Meteoroid flux and puncture models for cislunar space
Meteoroid and hypervelocity impact criteria for spacecraft design study
Meteoroid penetration measurements by Explorer XVI and XXIII satellites and Pegasus satellites for application to spacecraft design
Meteoroid protection system designs for optimum orbital space laboratories and manned interplanetary spacecraft